View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48783U 26145.57240867 +.00000000 +00000-0 +12306-3 0 00005
2 48783 87.9001 263.6834 0002061 124.4254 235.7072 13.15548217 03
| Epoch (UTC): | 25 May 2026 13:44:16 |
| Eccentricity: | 0.0002061 |
| inclination: | 87.9001° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6834° |
| argument of perigee: | 124.4254° |
| revolutions per day: | 13.15548217 |
| mean anomaly at epoch: | 235.7072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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